68A327138-2017: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.650 INCHES NOMINAL IN, overall_length: 5.290 INCHES NOMINAL IN, aircraft_location: NACELLE-VARIABLE INLET,OUTBOARD, material_thickness: 0.071 INCHES NOMINAL IN, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-337-8356, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY 2024 |
| overall_width | 2.650 INCHES NOMINAL IN |
| overall_length | 5.290 INCHES NOMINAL IN |
| aircraft_location | NACELLE-VARIABLE INLET,OUTBOARD |
| material_thickness | 0.071 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-337-8356 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4,T81 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 5.290 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.650 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.071 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | NACELLE-VARIABLE INLET,OUTBOARD |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.